US20080078227A1 - Sheet metal blank - Google Patents
Sheet metal blank Download PDFInfo
- Publication number
- US20080078227A1 US20080078227A1 US11/808,692 US80869207A US2008078227A1 US 20080078227 A1 US20080078227 A1 US 20080078227A1 US 80869207 A US80869207 A US 80869207A US 2008078227 A1 US2008078227 A1 US 2008078227A1
- Authority
- US
- United States
- Prior art keywords
- sheet metal
- metal blank
- raised
- casing
- thicker region
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 229910052751 metal Inorganic materials 0.000 title claims abstract description 73
- 239000002184 metal Substances 0.000 title claims abstract description 73
- 238000004519 manufacturing process Methods 0.000 claims abstract description 10
- 238000000034 method Methods 0.000 claims description 13
- 238000003754 machining Methods 0.000 claims description 4
- 239000000463 material Substances 0.000 claims description 3
- 238000004513 sizing Methods 0.000 claims description 3
- 238000003466 welding Methods 0.000 claims description 3
- 238000005304 joining Methods 0.000 claims description 2
- 238000003486 chemical etching Methods 0.000 claims 1
- 238000005096 rolling process Methods 0.000 description 5
- 238000005266 casting Methods 0.000 description 4
- 238000005242 forging Methods 0.000 description 4
- 238000005452 bending Methods 0.000 description 3
- 230000007704 transition Effects 0.000 description 2
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/84—Making other particular articles other parts for engines, e.g. connecting-rods
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J1/00—Preparing metal stock or similar ancillary operations prior, during or post forging, e.g. heating or cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/243—Flange connections; Bolting arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/403—Casings; Connections of working fluid especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/002—Wall structures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/26—Manufacture essentially without removing material by rolling
Definitions
- the invention relates to a sheet metal blank.
- the invention relates to a casing made from a sheet metal blank.
- Casings for gas turbine engines are frequently made from castings or forgings which are then machined to the correct dimensions.
- a casing may be fabricated from sheet metal, with end flanges and bosses being welded into place which are machined to final dimensions to interface with other components, to provide access to the engine when assembled, for the passage of pipes and services from the exterior of the interior of the engine (eg fuel pipes and cables) or to accept external fittings.
- the casings are typically very thin (perhaps only 1 to 5 mm thick) it is common for slight misalignments in the welding of the casing to result in damage to the casing.
- Modern engines frequently require a great many bosses on engine casings, and the consequential distortion due to welding at multiple locations can significantly affect the profile of the finished casing. Hence there is a high possibility of damage to the casing during the manufacturing process.
- each casing is formed from is as easily and cheaply produced as possible.
- a sheet metal blank for the manufacture of a casing of a gas turbine engine comprising a sheet of substantially constant wall thickness and at least one raised or thicker region extending along substantially the full length of the sheet metal blank, wherein at least one raised or thicker region is provided between edges of the sheet metal blank, said at least one raised or thicker region comprising at least one boss and at least one ridge extending away from the or each boss.
- the invention is a simple sheet metal structure from which the desired casing can be formed. It is advantageous to machine or otherwise form features of the finished product on sheet metal prior to forming into the final product shape as it is easier to machine a flat surface than, say, a curved surface. Machining a curved surface requires very close manufacturing tolerances to be observed and frequent base lining of machine tool co-ordinates to ensure correct positioning of the machine tool, which is not required to the same degree with machining a flat surface. Also if an error is made in machining the sheet metal then the cost of replacing the sheet metal is minimal compared to that of replacing a casting, forging or casing shell.
- a casing manufactured from a sheet metal blank herein described by a method of forming a casing as herein described.
- FIG. 1 shows a perspective view of a known casing (PRIOR ART);
- FIG. 2 shows a plan view of a sheet metal blank according to the present invention
- FIG. 3 shows a perspective view of a casing according to the present invention
- FIG. 4 shows a known rolling arrangement for bending the blank of the present invention
- FIG. 5 shows the casing in position on a sizing tool
- FIG. 6 shows a plan view of an alternative embodiment of a sheet metal blank according to the present invention.
- FIG. 1 PRIOR ART
- the casing 10 is frusto conical and may form an outer casing for a compressor or turbine module (not shown).
- the casing 10 is defined by a wall 12 which has a substantially constant thickness.
- the wall 12 is provided with a number of bosses 14 over its outer surface 15 , the bosses 14 being raised from the surface 15 such that the overall thickness of the casing 10 where a boss 14 is present is greater than the thickness of the wall 15 .
- Flanges 16 , 18 are provided at either end of the casing 10 for attachment to engine components upstream and downstream of the casing.
- the casing 10 may have been produced from a casting, or perhaps a forging where the bosses 14 and flanges 16 , 18 have been machined to their final dimensions. Alternatively it may have been produced from a plain sheet metal casing with bosses 14 welded into place on the surface 15 .
- the casing of the present invention is formed from a sheet metal blank 20 as shown in FIG. 2 .
- the blank 20 is in the form of a sector of a ring. That is to say it has a two curved parallel sides 22 , 24 and two ends 26 , 28 which are at an angle to one another but which both are perpendicular to a tangent at their junction with the curved sides 22 , 24 of the blank 20 .
- the blank 20 is formed from a sheet of metal of substantially constant wall thickness, which is then machined, chemical etched, forged, pressed or otherwise formed such that the resultant blank 20 has a wall 30 of substantially constant thickness and at least one raised or thicker region 32 extending along substantially the full length of the sheet metal blank 20 .
- flanges 34 , 36 are provided along both edges of the sheet metal blank form part for the raised/thicker region 32 . Further raised regions 32 are provided between edges 24 , 26 of the sheet metal blank 20 in the form of bosses 38 , and ridges 40 , where the ridges 40 extend away from each of the bosses 38 and/or link bosses 38 .
- the wall 30 has a thickness greater than 0.7 mm but not greater than 5 mm, and the raised regions 32 have a thickness no greater than twice the thickness of the wall 30 .
- the thicker regions 32 have substantially constant thickness along the full length of the blank.
- the bosses 38 and ridges 40 extends from one side of the wall 30 sheet metal blank, and the other side of the sheet metal blank wall 30 is planar.
- the sheet metal blank 20 , 80 is preferably made from titanium.
- bosses 38 may be linked to other bosses 38 by the ridges 40 .
- bosses may be provided in isolation with ridges 40 extending away from them for a distance.
- at all points along the length of the blank 20 there is at least one feature 32 which is raised above the wall surface 30 .
- the ridges 40 In the region where the ridges 40 meet the bosses 38 , the ridges 40 splay out so as to provide a lead in to the bosses 38 . That is to say, the ridges 40 run onto the crown of the bosses 38 such that the there is a gradual change in width of the raised feature 32 in the transition between the ridge 40 and the bosses 38 .
- FIG. 3 shows a casing 50 formed from the sheet metal blank 20 of FIG. 2 .
- the blank 20 is deformed such that it is substantially circular in cross-section and then joined at the ends 26 , 28 to form the frusto conical casing 50 .
- the sheet metal blank 20 is joined at ends 26 , 28 by a weld 52 .
- the sheet metal blank 20 is deformed by a process known as rolling, as illustrated in FIG. 4 , in which the blank 20 is passed along a series of rollers 60 , 62 , 64 , the through path defined by the rollers 60 , 62 , 64 being wider than the thickness of the wall 30 of the sheet 20 (shown as a dotted line in FIG. 4 ), but narrower than the thickness of the thicker region 32 .
- the distance between the rollers 60 , 62 , 64 is fixed during the rolling operation, hence the rollers 60 , 62 , 64 do not contact the metal blank 20 at its thinnest regions on both sides of wall 30 .
- the raised regions 32 ensure the sheet metal blank 20 is in contact with the rollers 60 , 62 , 64 throughout the bending process such that the sheet metal blank 20 is bent along substantially its full length to form an arcuate sheet.
- the arcuate sheet is then is joined at its ends 26 , 28 to form a casing 50 with a substantially circular cross section.
- the casing 50 may then optionally be further formed by being placed on a jig 70 and stretched either expansion of the jig and/or by being forced down the conical surface of the jig 70 .
- Such stretching enables the final dimensions of the casing 50 to achieved. That is to say, after the ends 26 , 28 are joined the casing 50 may not have the desired cross section at all points along its length, and the optional stretching step will ensure the design dimensions are achieved.
- Some or all of the bosses 38 may then be machined to produce a flat location surface.
- a rectangular sheet metal blank 80 may be produced rather than the arcuate blank 20 shown in FIG. 2 .
- features of the blank 80 and method of manufacture of the blank and resultant casing are common to the blank 20 .
- the blank 20 , 80 and casing 50 are described as having a plurality of bosses 38 and ridges 40 .
- bosses are not required, only ridges and/or a flange extending along the full length of the blank 28 , 80 are provided.
- a blank 20 , 80 may be provided with a single boss 38 and/or a single ridge 40 extending away from the boss 38 .
- the raised region 32 extends substantially along the full length of the sheet metal blank 20 , 80 .
- lead in features at the ends 26 , 28 of the blank 20 , 80 may be provided which have either no raised region 32 , or a tapered raised region. These will help to feed the blank into to rolling/bending device.
- the splayed ends of the ridges 40 in the transition region between the ridges 40 and the bosses 38 also act as a lead in for each boss 38 between the rollers ( 60 , 62 , 64 ), thus reducing the occurrence of an uneven residual stress in the region of the boss 38 when bent.
- the casing is manufactured from one piece of sheet metal.
- the casing is made from two or more deformed sheet metal blanks, which are then joined together to form one substantially cylindrical or frusto-conical shape.
- the method of deforming the sheet metal blank such that it is substantially arcuate or circular in cross section may be achieved by use of a press brake rather than by rolling.
- sheet metal where a “sheet” is intended to described a material provided in a substantially flat and plane form.
- sheet metal is exchangeable with “plate metal”, another term of the art, which is indicative of a material which is provided in a thicker form than a “sheet”.
- the raised or thicker regions 32 have a width of no less than 7 mm. In a titanium alloy casing this has been shown to distribute stress around the features of the thicker region to within optimal limits.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Forging (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
Abstract
Description
- The invention relates to a sheet metal blank.
- In particular the invention relates to a casing made from a sheet metal blank.
- Casings for gas turbine engines, for example compressor outer casings, combustor outer casings and turbine outer casings, are frequently made from castings or forgings which are then machined to the correct dimensions. Alternatively a casing may be fabricated from sheet metal, with end flanges and bosses being welded into place which are machined to final dimensions to interface with other components, to provide access to the engine when assembled, for the passage of pipes and services from the exterior of the interior of the engine (eg fuel pipes and cables) or to accept external fittings. Since the casings are typically very thin (perhaps only 1 to 5 mm thick) it is common for slight misalignments in the welding of the casing to result in damage to the casing. Modern engines frequently require a great many bosses on engine casings, and the consequential distortion due to welding at multiple locations can significantly affect the profile of the finished casing. Hence there is a high possibility of damage to the casing during the manufacturing process.
- Hence a casing having the required number of features, strength and geometry which can be produced by a method resulting in less component rejections is highly desirable.
- The production of the base casting, forging or sheet metal shell to which bosses are welded to is also a problematic process and results in many rejections, slowing the manufacturing process and increasing the over all cost of each component which is successfully produced.
- Hence it is desirable that the base structure that each casing is formed from is as easily and cheaply produced as possible.
- According to a first aspect of the invention there is provided a sheet metal blank for the manufacture of a casing of a gas turbine engine, comprising a sheet of substantially constant wall thickness and at least one raised or thicker region extending along substantially the full length of the sheet metal blank, wherein at least one raised or thicker region is provided between edges of the sheet metal blank, said at least one raised or thicker region comprising at least one boss and at least one ridge extending away from the or each boss.
- Thus the invention is a simple sheet metal structure from which the desired casing can be formed. It is advantageous to machine or otherwise form features of the finished product on sheet metal prior to forming into the final product shape as it is easier to machine a flat surface than, say, a curved surface. Machining a curved surface requires very close manufacturing tolerances to be observed and frequent base lining of machine tool co-ordinates to ensure correct positioning of the machine tool, which is not required to the same degree with machining a flat surface. Also if an error is made in machining the sheet metal then the cost of replacing the sheet metal is minimal compared to that of replacing a casting, forging or casing shell.
- According to a second aspect of the invention there is provided a method of forming a casing comprising the steps of:
-
- a) manufacturing a sheet metal blank as herein described having two sides and two ends;
- b) deforming the sheet metal blank such that it is substantially circular in cross-section; and
- c) joining the sheet metal blank at its ends;
wherein the sheet metal blank is deformed by passing it along a series of rollers, the through path defined by the rollers being wider than the thickness of the sheet wall and narrower that the thickness of the at least one raised or thicker region. Thus when the sheet metal blank passes through the rollers, the rollers are always in contact with raised or thicker regions.
- According to a second aspect of the invention there is provided a casing manufactured from a sheet metal blank herein described by a method of forming a casing as herein described.
- The invention will now be described by way of example only with reference to the accompanying drawings in which:
-
FIG. 1 shows a perspective view of a known casing (PRIOR ART); -
FIG. 2 shows a plan view of a sheet metal blank according to the present invention; -
FIG. 3 shows a perspective view of a casing according to the present invention; -
FIG. 4 shows a known rolling arrangement for bending the blank of the present invention; -
FIG. 5 shows the casing in position on a sizing tool; and -
FIG. 6 shows a plan view of an alternative embodiment of a sheet metal blank according to the present invention. - Presented in
FIG. 1 (PRIOR ART) is a perspective view of a known casing 10. The casing 10 is frusto conical and may form an outer casing for a compressor or turbine module (not shown). The casing 10 is defined by awall 12 which has a substantially constant thickness. Thewall 12 is provided with a number ofbosses 14 over itsouter surface 15, thebosses 14 being raised from thesurface 15 such that the overall thickness of the casing 10 where aboss 14 is present is greater than the thickness of thewall 15.Flanges bosses 14 andflanges bosses 14 welded into place on thesurface 15. - In contrast the casing of the present invention is formed from a sheet metal blank 20 as shown in
FIG. 2 . The blank 20 is in the form of a sector of a ring. That is to say it has a two curvedparallel sides ends curved sides wall 30 of substantially constant thickness and at least one raised orthicker region 32 extending along substantially the full length of the sheet metal blank 20. In the embodiment shownflanges thicker region 32. Further raisedregions 32 are provided betweenedges ridges 40, where theridges 40 extend away from each of the bosses 38 and/or link bosses 38. - The
wall 30 has a thickness greater than 0.7 mm but not greater than 5 mm, and the raisedregions 32 have a thickness no greater than twice the thickness of thewall 30. Thethicker regions 32 have substantially constant thickness along the full length of the blank. The bosses 38 andridges 40 extends from one side of thewall 30 sheet metal blank, and the other side of the sheet metalblank wall 30 is planar. The sheet metal blank 20, 80 is preferably made from titanium. - As shown in
FIG. 2 , the bosses 38 may be linked to other bosses 38 by theridges 40. Alternatively bosses may be provided in isolation withridges 40 extending away from them for a distance. However, at all points along the length of the blank 20 there is at least onefeature 32 which is raised above thewall surface 30. - In the region where the
ridges 40 meet the bosses 38, theridges 40 splay out so as to provide a lead in to the bosses 38. That is to say, theridges 40 run onto the crown of the bosses 38 such that the there is a gradual change in width of the raisedfeature 32 in the transition between theridge 40 and the bosses 38. -
FIG. 3 shows acasing 50 formed from the sheet metal blank 20 ofFIG. 2 . The blank 20 is deformed such that it is substantially circular in cross-section and then joined at theends conical casing 50. The sheet metal blank 20 is joined atends weld 52. - The sheet metal blank 20 is deformed by a process known as rolling, as illustrated in
FIG. 4 , in which the blank 20 is passed along a series ofrollers rollers wall 30 of the sheet 20 (shown as a dotted line inFIG. 4 ), but narrower than the thickness of thethicker region 32. The distance between therollers rollers wall 30. The raised regions 32 (that is to say, theridges 40 extending away from and between the bosses 38 and/or theflanges 34, 36) ensure the sheet metal blank 20 is in contact with therollers ends casing 50 with a substantially circular cross section. - As shown in
FIG. 5 thecasing 50 may then optionally be further formed by being placed on ajig 70 and stretched either expansion of the jig and/or by being forced down the conical surface of thejig 70. Such stretching enables the final dimensions of thecasing 50 to achieved. That is to say, after theends casing 50 may not have the desired cross section at all points along its length, and the optional stretching step will ensure the design dimensions are achieved. Some or all of the bosses 38 may then be machined to produce a flat location surface. - In an alternative embodiment, where a cylindrical rather than frusto-conical casing is required, a rectangular sheet metal blank 80, as shown in
FIG. 6 , may be produced rather than the arcuate blank 20 shown inFIG. 2 . Other than the rectangular shape, features of the blank 80 and method of manufacture of the blank and resultant casing are common to the blank 20. - In the embodiments herein described the blank 20, 80 and
casing 50 are described as having a plurality of bosses 38 andridges 40. However, in an application where bosses are not required, only ridges and/or a flange extending along the full length of the blank 28, 80 are provided. Alternatively a blank 20, 80 may be provided with a single boss 38 and/or asingle ridge 40 extending away from the boss 38. - The raised
region 32 extends substantially along the full length of the sheet metal blank 20, 80. However, lead in features at theends region 32, or a tapered raised region. These will help to feed the blank into to rolling/bending device. - The splayed ends of the
ridges 40 in the transition region between theridges 40 and the bosses 38 also act as a lead in for each boss 38 between the rollers (60, 62, 64), thus reducing the occurrence of an uneven residual stress in the region of the boss 38 when bent. - In the embodiment described above, the casing is manufactured from one piece of sheet metal. In an alternative embodiment, the casing is made from two or more deformed sheet metal blanks, which are then joined together to form one substantially cylindrical or frusto-conical shape.
- The method of deforming the sheet metal blank such that it is substantially arcuate or circular in cross section may be achieved by use of a press brake rather than by rolling.
- Reference is hereinbefore made to sheet metal, where a “sheet” is intended to described a material provided in a substantially flat and plane form. In this context “sheet metal” is exchangeable with “plate metal”, another term of the art, which is indicative of a material which is provided in a thicker form than a “sheet”.
- The raised or
thicker regions 32 have a width of no less than 7 mm. In a titanium alloy casing this has been shown to distribute stress around the features of the thicker region to within optimal limits. - Providing a casing with thicker/raised regions extending between bosses is counterintuitive, as it will be appreciated that ordinarily such features act a stress concentration features. It is only with careful positioning, sizing and shaping that the raised features can be “tuned” to produce a structure which is more rigid than that of the prior art (since the thicker/raised regions stiffen the casing) and which results in a component with stress concentrations that are within acceptable limits.
Claims (14)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0619361A GB2442238B (en) | 2006-09-29 | 2006-09-29 | Sheet metal blank |
GB0619361.9 | 2006-09-29 |
Publications (2)
Publication Number | Publication Date |
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US20080078227A1 true US20080078227A1 (en) | 2008-04-03 |
US9003852B2 US9003852B2 (en) | 2015-04-14 |
Family
ID=37435025
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US11/808,692 Active 2032-02-13 US9003852B2 (en) | 2006-09-29 | 2007-06-12 | Sheet metal blank |
Country Status (2)
Country | Link |
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US (1) | US9003852B2 (en) |
GB (1) | GB2442238B (en) |
Cited By (2)
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WO2014052967A1 (en) * | 2012-09-28 | 2014-04-03 | United Technologies Corporation | Case assembly for a gas turbine engine |
WO2015175076A3 (en) * | 2014-02-19 | 2016-01-14 | United Technologies Corporation | Reduced stress boss geometry for a gas turbine engine |
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US9498850B2 (en) | 2012-03-27 | 2016-11-22 | Pratt & Whitney Canada Corp. | Structural case for aircraft gas turbine engine |
US20170362960A1 (en) * | 2016-06-21 | 2017-12-21 | United Technologies Corporation | Turbine case boss |
GB2553531B (en) | 2016-09-07 | 2019-02-06 | Rolls Royce Plc | A method of attaching a projection to a thin walled component |
US10808574B2 (en) * | 2016-09-13 | 2020-10-20 | General Electric Company | Turbomachine stator travelling wave inhibitor |
US12158076B1 (en) * | 2023-07-07 | 2024-12-03 | Pratt & Whitney Canada Corp. | Local stiffening for gas turbine engine casing |
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WO2015175076A3 (en) * | 2014-02-19 | 2016-01-14 | United Technologies Corporation | Reduced stress boss geometry for a gas turbine engine |
US10458333B2 (en) | 2014-02-19 | 2019-10-29 | United Technologies Corporation | Reduced stress boss geometry for a gas turbine engine |
US11208955B2 (en) | 2014-02-19 | 2021-12-28 | Raytheon Technologies Corporation | Reduced stress boss geometry for a gas turbine engine |
Also Published As
Publication number | Publication date |
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US9003852B2 (en) | 2015-04-14 |
GB0619361D0 (en) | 2006-11-08 |
GB2442238A (en) | 2008-04-02 |
GB2442238B (en) | 2008-10-01 |
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